Inlet Geometry Effects on the Internal Performance of a Variable Flow Ducted Rocket Combustor
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
2013-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Inlet Geometry Effects on the Flowfield of a Ducted Rocket Combustor
British Library Conference Proceedings | 2013
|Performance Prediction of a Variable Flow Ducted Rocket Combustor
British Library Conference Proceedings | 2013
|Modelling combustor performance of a ducted rocket
AIAA | 2000
|